1
0
Fork 0

Sync. with JSBSim

This commit is contained in:
ehofman 2009-07-29 13:50:39 +00:00 committed by Tim Moore
parent 94caa0b891
commit a7976b835d
6 changed files with 42 additions and 26 deletions

View file

@ -58,7 +58,8 @@ FGState::FGState(FGFDMExec* fdex)
FDMExec = fdex; FDMExec = fdex;
sim_time = 0.0; sim_time = 0.0;
//dt = 1.0/120.0; dt = 1.0/120.0; // a default timestep size. This is needed for when JSBSim is
// run in standalone mode with no initialization file.
Aircraft = FDMExec->GetAircraft(); Aircraft = FDMExec->GetAircraft();
Propagate = FDMExec->GetPropagate(); Propagate = FDMExec->GetPropagate();

View file

@ -35,14 +35,9 @@ SENTRY
INCLUDES INCLUDES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#ifdef HAVE_CONFIG_H
# include <config.h>
#endif
#include <string> #include <string>
#include <iostream> #include <iostream>
#include <simgear/props/props.hxx> #include "simgear/props/props.hxx"
#include <simgear/math/SGMath.hxx>
#include "FGJSBBase.h" #include "FGJSBBase.h"

View file

@ -310,6 +310,19 @@ FGColumnVector3& FGLGear::Force(void)
RollingForce = ((1.0 - TirePressureNorm) * 30 + vLocalForce(eZ) * BrakeFCoeff) * sign; RollingForce = ((1.0 - TirePressureNorm) * 30 + vLocalForce(eZ) * BrakeFCoeff) * sign;
SideForce = vLocalForce(eZ) * FCoeff; SideForce = vLocalForce(eZ) * FCoeff;
// Lag and attenuate the XY-plane forces dependent on velocity. This code
// uses a lag filter, C/(s + C) where "C" is the filter coefficient. When
// "C" is chosen at the frame rate (in Hz), the jittering is significantly
// reduced. This is because the jitter is present *at* the execution rate.
// If a coefficient is set to something equal to or less than zero, the
// filter is bypassed.
if (LongForceLagFilterCoeff > 0) RollingForce = LongForceFilter.execute(RollingForce);
if (LatForceLagFilterCoeff > 0) SideForce = LatForceFilter.execute(SideForce);
if ((fabs(RollingWhlVel) <= RFRV) && RFRV > 0) RollingForce *= fabs(RollingWhlVel)/RFRV;
if ((fabs(SideWhlVel) <= SFRV) && SFRV > 0) SideForce *= fabs(SideWhlVel)/SFRV;
// Transform these forces back to the local reference frame. // Transform these forces back to the local reference frame.
vLocalForce(eX) = RollingForce*CosWheel - SideForce*SinWheel; vLocalForce(eX) = RollingForce*CosWheel - SideForce*SinWheel;
@ -319,19 +332,6 @@ FGColumnVector3& FGLGear::Force(void)
vForce = Propagate->GetTl2b() * vLocalForce; vForce = Propagate->GetTl2b() * vLocalForce;
// Lag and attenuate the XY-plane forces dependent on velocity. This code
// uses a lag filter, C/(s + C) where "C" is the filter coefficient. When
// "C" is chosen at the frame rate (in Hz), the jittering is significantly
// reduced. This is because the jitter is present *at* the execution rate.
// If a coefficient is set to something equal to or less than zero, the
// filter is bypassed.
if (LongForceLagFilterCoeff > 0) vForce(eX) = LongForceFilter.execute(vForce(eX));
if (LatForceLagFilterCoeff > 0) vForce(eY) = LatForceFilter.execute(vForce(eY));
if ((fabs(RollingWhlVel) <= RFRV) && RFRV > 0) vForce(eX) *= fabs(RollingWhlVel)/RFRV;
if ((fabs(SideWhlVel) <= SFRV) && SFRV > 0) vForce(eY) *= fabs(SideWhlVel)/SFRV;
// End section for attentuating gear jitter // End section for attentuating gear jitter
vMoment = vWhlBodyVec * vForce; vMoment = vWhlBodyVec * vForce;
@ -340,9 +340,14 @@ FGColumnVector3& FGLGear::Force(void)
WOW = false; WOW = false;
compressLength = 0.0; compressLength = 0.0;
compressSpeed = 0.0;
// No wheel conditons // No wheel conditions
RollingWhlVel = SideWhlVel = WheelSlip = 0.0; SideWhlVel = WheelSlip = 0.0;
// Let wheel spin down slowly
RollingWhlVel -= 13.0*dT;
if (RollingWhlVel < 0.0) RollingWhlVel = 0.0;
// Return to neutral position between 1.0 and 0.8 gear pos. // Return to neutral position between 1.0 and 0.8 gear pos.
SteerAngle *= max(GetGearUnitPos()-0.8, 0.0)/0.2; SteerAngle *= max(GetGearUnitPos()-0.8, 0.0)/0.2;
@ -371,6 +376,7 @@ void FGLGear::ComputeRetractionState(void)
GearUp = true; GearUp = true;
WOW = false; WOW = false;
GearDown = false; GearDown = false;
RollingWhlVel = 0.0;
} else if (gearPos > 0.99) { } else if (gearPos > 0.99) {
GearDown = true; GearDown = true;
GearUp = false; GearUp = false;

View file

@ -94,14 +94,24 @@ double FGElectric::Calculate(void)
string FGElectric::GetEngineLabels(string delimeter) string FGElectric::GetEngineLabels(string delimeter)
{ {
return ""; // currently no labels are returned for this engine std::ostringstream buf;
buf << Name << " HP (engine " << EngineNumber << ")" << delimeter
<< Thruster->GetThrusterLabels(EngineNumber, delimeter);
return buf.str();
} }
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
string FGElectric::GetEngineValues(string delimeter) string FGElectric::GetEngineValues(string delimeter)
{ {
return ""; // currently no values are returned for this engine std::ostringstream buf;
buf << HP << delimeter
<< Thruster->GetThrusterValues(EngineNumber, delimeter);
return buf.str();
} }
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

View file

@ -199,6 +199,8 @@ double FGPropeller::Calculate(double PowerAvailable)
vH(eY) = 0.0; vH(eY) = 0.0;
vH(eZ) = 0.0; vH(eZ) = 0.0;
vH = Transform()*vH; // Transform rotational momentum to rotated frame (if any)
if (omega > 0.0) ExcessTorque = GearRatio * PowerAvailable / omega; if (omega > 0.0) ExcessTorque = GearRatio * PowerAvailable / omega;
else ExcessTorque = GearRatio * PowerAvailable / 1.0; else ExcessTorque = GearRatio * PowerAvailable / 1.0;
@ -206,7 +208,9 @@ double FGPropeller::Calculate(double PowerAvailable)
if (RPM < 1.0) RPM = 0; // Engine friction stops rotation arbitrarily at 1 RPM. if (RPM < 1.0) RPM = 0; // Engine friction stops rotation arbitrarily at 1 RPM.
vMn = fdmex->GetPropagate()->GetPQR()*vH + vTorque; // Transform Torque and momentum prior to this equation, as PQR is used in this
// equation and cannot be transformed itself.
vMn = fdmex->GetPropagate()->GetPQR()*vH + Transform()*vTorque;
return Thrust; // return thrust in pounds return Thrust; // return thrust in pounds
} }

View file

@ -91,7 +91,7 @@ bool FGTurboProp::Load(FGFDMExec* exec, Element *el)
if (el->FindElement("idlen1")) if (el->FindElement("idlen1"))
IdleN1 = el->FindElementValueAsNumber("idlen1"); IdleN1 = el->FindElementValueAsNumber("idlen1");
if (el->FindElement("idlen2")) if (el->FindElement("idlen2"))
IdleN2 = el->FindElementValueAsNumber("idlen1"); IdleN2 = el->FindElementValueAsNumber("idlen2");
if (el->FindElement("maxn1")) if (el->FindElement("maxn1"))
MaxN1 = el->FindElementValueAsNumber("maxn1"); MaxN1 = el->FindElementValueAsNumber("maxn1");
if (el->FindElement("maxn2")) if (el->FindElement("maxn2"))